A single vibrating tube transducer comprises a tube (4) held between two nodal masses (6) which are attached to the tube (2) close to their respective centers of gravity (16). Each nodel mass (6) has an extended portion (14) which is attached at its free end to the opposing nodal mass by an arrangement of metal ligaments (18). Vibrating means (19) and sensing means (20) drive and detect the tube motion respectively. The tube has discontinuities (28) adjacent to the vibrating means (19) and the sensing means (20), to ensure the desired mode of resonance is achieved. Acoustic baffles (30) prevent inaccuracies due to internal acoustic resonance in the transducer.
|
11. A single vibrating tube transducer comprising a straight tube through which a fluid to be measured flows, means for vibrating the tube, at least one means for sensing the vibrations of the tube wherein the tube is of uniform circular section except for at least one flat which is machined on its external surface at at least one desired anti-node on the tube.
9. A single vibrating tube transducer comprising a straight tube through which a fluid to be measured flows, means for vibrating the tube, at least one means for sensing vibrations of the tube and first and second nodal masses attached to respective ends of the tube, wherein the tube is shrouded within extended portions of the nodal masses, which create an annular gap between the extended portions and the tube, and wherein at least one acoustic baffle is inserted within said gap.
6. A single vibrating tube transducer comprising a straight tube through which a fluid to be measured flows, means for vibrating the tube, at least one means for sensing the vibrations of the tube and first and second nodal masses attached to respective ends of the tube, wherein each nodal mass extends substantially the length of the tube, the two extended portions being on opposing sides of the tube, and each extended portion being linked to the opposing nodal mass close to the point of attachment of the said opposing nodal mass.
1. A single vibrating tube transducer comprising a straight tube through which a fluid to be measured flows, first and second nodal masses attached to respective ends of the tube, means for vibrating the tube, and at least one means for sensing the vibrations of the tube, wherein each nodal mass has a first extended portion extending alongside the tube towards the other nodal mass and a second oppositely extending portion counterbalancing the first portion and rendering the centre of gravity proximal to the point of attachment of the mass to the tube.
2. A transducer according to
3. A transducer according to
4. A transducer according to
5. A transducer according to
7. A transducer according to
8. A transducer according to
10. A transducer according to
12. A transducer according to
13. A transducer according to
14. A transducer according to
|
This invention relates to single vibrating tube transducers which are typically used to measure mass, density, or mass flow.
Transducers of this kind are very well known. One example is described in our patent specification GB No. 2 062 865. Such transducers exploit the well known fact that fluid flowing in a vibrating tube which is clamped at its two ends will produce a phase difference between the transverse displacements of the upstream and downstream ends of the tube. The mass flow rate of a fluid in such a tube is a linear function of the ratio A of the phase difference to the resonant frequency of the tube, where
A=φ/F
φ being the phase difference and F being the resonant frequency of the tube. The mass flow rate M is then give by
M=a A+b
where a and b are constants and are independent of the fluid type and flow rate.
Transducers of this type are subject to variations in accuracy due to external vibrations and shocks when they are used in hazardous environments. Problems have also been encountered due to the vibrating tube setting up an acoustic resonance between the tube and the instrument casing. Another problem is the fact that antinodes of vibration may be set up at points on the tube distant from the means for sensing the vibrations and will thus cause inaccuracies in phase difference measurement.
Known measures (GB No. 2 062 865) for overcoming some of these problems include slight ellipticity of the tube to define the vibrational mode; this imposes manufacturing problems. The nodes are typically clamped by nodal masses and in GB No. 2 062 865 these masses are extended towards each other around the vibrating tube and connected by a flexible bellows to form a sealed enclosure which can be evacuated to present contamination of the components by dust etc. which may cause inaccuracies. Maintenance of an evacuated enclosure imposes problems in use. Moreover the extended nodal masses have a centre of gravity displaced from the nodal point of attachment to the tube and shocks can be communicated to the tube too easily.
The object of the present invention is to provide more satisfactory solutions to the problems dealt with above.
The present invention is defined in the appended claims to which reference should now be made.
FIG. 1 is a longitudinal cross-section through a transducer embodying the invention;
FIG. 2 is an axial view of a connection between the two nodal masses in this embodiment of the invention;
FIG. 3 is a side view of the connections between the two nodal masses in this embodiment of the invention; and
FIG. 4 illustrates a preferred embodiment of the drive means for vibrating the tube.
The transducer shown in FIG. 1 is protected from damage by a cylindrical casing 2. Mounted centrally in the casing 2 is a generally cylindrical tube 4 through which the fluid to be measured passes. Each end of the tube 4 passes through a nodal mass 6 and is rigidly attached thereto by two circumferential welds 8, one on either axial side of an inner annular portion 6a of the nodal mass closely fitting on the tube 4.
The ends of the tube 4 are connected to cylindrical bellows 10 which absorb the thermal expansion of the tube and the external pipes, and also protect the tube from noise and vibration in the external pipes. The bellows are connected to flange pieces 12 which seal the ends of the casing 2 and also provide means to connect the transducer into a main line.
The two nodal masses 6 have arcuate extended portions 14 which run substantially the length of the tube 2, preferably on opposing sides of the tube. These are welded to the inner annular portion 6a once it has been welded to the tube. A typical cross-section through one of these extended portions 14 can be seen in FIG. 2. Each nodal mass has its weight distributed in such a way that its centre of gravity 16 is on the axis of the tube 4 and axially between the two welds 8 attaching it to the tube 4.
To this end, each cantilevered extension 4 is counterbalanced by a sleeve extension 15 rearwardly cantilevered from the inner annular portion 6a. The extension 15 is welded to the inner annular portion once it has been welded to the tube. This ensures that any movement of the instrument due to plant vibration or shock will not impose excessive stresses in the vibrating tube, which would cause the transducer to give inaccurate readings.
The double weld 8 attaching each nodal mass 6 to the tube 4 helps to protect the tube 4 against transverse shocks by reducing the tendency of the nodal mass to pivot when the transducer is subjected to transverse shocks. The fact that the nodal masses are in three or more sections enables this double weld to be made relatively easily since the inner annular portions 6a can be easily accessed before the cantilevered sections 14 and 15 are welded on.
The end of the extended portion 14 of each nodal mass is linked to the opposing nodal mass by an arrangement of thin metal strip ligaments 18, as illustrated in FIG. 2 and FIG. 3. In this embodiment, four ligaments 18 are used and are so arranged that at least one of them is always in tension when the transducer is subject to transverse shocks and vibrations, i.e., the link arrangement is rigid transversely. The links do however allow for axial movement of the nodal masses. This linking together of the nodal masses substantially increases their inertial mass which helps to keep the ends of the tube stationary when the tube is vibrating.
In order to ensure that at least one link 18 is always in tension, they are arranged in two crossing pairs but the points of attachment of their ends are transversely offset in such a way that the links do not touch where they cross. In the arrangement of FIGS. 2 and 3, the nodal masses each have a transversely extending first arcuate section 6b fixed to the inner annular section 6a and a second arcuate section 6c fixed between the inner annular section and the extended portion 14 on the opposite side of the tube to the first arcuate section 6b. The extended portion 14 has a third arcuate section 14a at its distal end. A first pair of ligaments is welded at one end to the first arcuate section 6b and at the other end each is welded to opposite ends of the third arcuate section 14a. A second pair of ligaments extends from the centre of the third arcuate section 14a to opposite ends of the second arcuate section 6c. Thus the two pairs of ligaments are transversely offset and do not touch when they cross and whatever the relative movement of the two nodal masses, at least one ligament will always be in tension.
To ensure that one ligament 18 is always in tension a minimum of two are required, but the arrangement described here with four ligaments is more rigid.
Mounted on the extended portions 14 of the two nodal masses are the vibrating means 19 to drive the tube at a central anti-node and the sensing means 20 at further anti-nodes on the tube to detect the vibrations of the tube. In the embodiment shown here the vibrating means and sensing means are in pairs on either side of the tube, one from each pair being fixed to each nodal mass.
The vibrating means and the sensing means for this embodiment are shown in FIG. 4. They comprise a permanent magnet 22 with its axis perpendicular to the wall of the tube. An electric coil 24 is wound round the magnet. The magnet has a small gap 26 of around 0.1 mm between it and the tube which is made from a magnetic material. An alternating voltage is applied to the coil which produces an alternating magnetic field in the gap 26 which causes the magnetic tube to vibrate at the frequency of the alternating voltage. With a drive means on either side of the tube as is the case with this embodiment, the polarities of the two coils are reversed so thay they are both moving the tube in the same direction at the same time.
The same device can be used for the sensing means. The natural resonant vibration of the magnetic tube in the gap 26 produces an a.c. voltage on the coil 24. The frequency of this a.c. voltage is equal to the frequency of vibration of the tube. The vibrations are self sustaining having been triggered by s small purturbation. They are sustained by a positive feedback loop between the pick-up coils and the drive coils. When the transducer is used to measure density, only one set of pick-up coils is required to measure the frequency of vibration.
The vibrating means and the sensing means are controlled by a control circuit 28 located within an external housing 30. This has a power input/signal output connection 32. For mass flow measurements, the control circuit evaluates the phase difference between the two sensing means locations on the tube in a manner similar to that described in our British patent application no. 86 17415.
In the embodiment shown here the vibrating weans is mounted equidistantly from the two nodal masses and the two sensing means are located symmetrically about the vibrating means.
The vibrating means 19 is located at an anti-node halfway between the two nodal masses. In this embodiment there are two further anti-nodes between each nodal mass 6 and the vibrating means 19.
Adjacent to each vibrating means and each sensing means, material has been removed to produce a localised flat surface 28. These flat surfaces, which reduce the tube stiffness at that point, ensure a mode of vibration with these positions as anti-nodes. These flats 28 also improve the performance of the vibrating means and sensing means since the gap 26 between the flat end of each magnet pole piece and the tube is now parallel.
Other discontinuities could be introduced to the tube at these locations to ensure that they become anti-nodes, and this may involve the addition instead of the removal of material.
Also attached to the extended portions 14 of the nodal masses are acoustic baffles 30. These baffles 30 are between the tube and the nodal masses but do not contact the tube. The purpose of these baffles is to prevent any acoustic resonance within the transducer casing without having to evacuate the tube of gas. This resonance would affect the vibration of the tube and cause inaccuracies in measurement. The baffles are typically made from a foamed plastics material or a honeycomb composite material. This type of material has good acoustic absorption properties because of the voids in its structure.
The improvements described above are intended to be applied to any type of vibrating tube transducer. The improvements provide a transducer which is much less susceptible to external shocks and vibrations, which has its resonant mode better defined, and which is not subject to inaccuracy due to internal acoustic resonance.
The transducer described here is one embodiment of the invention and variations in this are possible. For example, the extended portions of the nodal masses need not be arcuate and could in fact have any cross-section. A rectangular cross-section would be advantageous in increasing the stiffness thereof. If used with the density transducer of our GB No. 2 062 865 they might be elliptical for use with an elliptical tube. The linkages between nodal masses could have a larger number of ligaments in order to add rigidity.
Stansfeld, James W., Atkinson, David I. H.
Patent | Priority | Assignee | Title |
10107784, | Dec 29 2014 | Concentric Meter Corporation | Electromagnetic transducer |
10126266, | Dec 29 2014 | Concentric Meter Corporation | Fluid parameter sensor and meter |
10533884, | Dec 18 2014 | Endress + Hauser Flowtec AG | Measuring transducer of vibration-type |
5261284, | Oct 13 1992 | Micro Motion, Incorporated | Non-interacting enclosure design for coriolis mass flow meters |
5323658, | Jun 19 1992 | Fuji Electric Co., Ltd. | Coriolis mass flowmeter |
5365794, | Jul 22 1991 | Krohne, AG | Mass flow meter |
5476013, | Jul 22 1991 | Krohne AG | Mass flow meter |
5503028, | Jul 09 1993 | Facom | Tool for measuring torque, such as an electronic dynamometer wrench |
5549009, | Sep 04 1990 | Endress + Hauser Flowtec AG | Apparatus for determining and dosing mass flows |
5691485, | Jun 06 1994 | Oval Corporation | Coaxial double tube type Coriolis flowmeter |
5974858, | May 02 1997 | CALIBRON SYSTEMS, INC | Single flange installation densimeter |
5979246, | Feb 09 1998 | Micro Motion, Inc.; Micro Motion, Inc | Spring rate balancing of the flow tube and a balance bar in a straight tube Coriolis flowmeter |
6170339, | Oct 07 1997 | Krohne AG | Coriolis mass flowmeter |
9523272, | Dec 28 2013 | Halliburton Energy Services, Inc | Amplification of data-encoded sound waves within a resonant area |
9752911, | Dec 29 2014 | Concentric Meter Corporation | Fluid parameter sensor and meter |
Patent | Priority | Assignee | Title |
3585843, | |||
4760744, | Sep 26 1985 | Danfoss A/S | Mass flow meter based on the coriolis principle |
4823614, | Apr 28 1986 | Coriolis-type mass flowmeter |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Nov 08 1988 | STANSFELD, JAMES WOLRYCHE | Schlumberger Industries Limited | ASSIGNMENT OF ASSIGNORS INTEREST | 004971 | /0170 | |
Nov 08 1988 | ATKINSON, DAVID IAN HEATON | Schlumberger Industries Limited | ASSIGNMENT OF ASSIGNORS INTEREST | 004971 | /0170 | |
Nov 18 1988 | Schlumberger Industries Limited | (assignment on the face of the patent) | / | |||
Nov 09 1994 | Solartron Electronic Group Limited | Schlumberger Industries Limited | CHANGE OF NAME SEE DOCUMENT FOR DETAILS | 007417 | /0242 | |
Nov 09 1994 | SCHLUMBERGER ELECTRONICS U K LIMITED | Schlumberger Industries Limited | CHANGE OF NAME SEE DOCUMENT FOR DETAILS | 007417 | /0242 | |
Mar 03 1995 | Schlumberger Industries Limited | SOLARTRON GROUP LIMITED A COMPANY ORGANIZED UNDER THE LAWS OF ENGLAND | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 007417 | /0229 | |
May 20 2003 | WESTON AEROSPACE 2003 LIMITED | SOLARTRON MOBREY LIMITED | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 016522 | /0374 | |
May 24 2004 | Solartron Group Limited | WESTON AEROSPACE 2003 LIMITED | CHANGE OF NAME SEE DOCUMENT FOR DETAILS | 016851 | /0377 |
Date | Maintenance Fee Events |
Apr 14 1994 | M183: Payment of Maintenance Fee, 4th Year, Large Entity. |
May 09 1994 | ASPN: Payor Number Assigned. |
Mar 20 1998 | M184: Payment of Maintenance Fee, 8th Year, Large Entity. |
Mar 21 2002 | M185: Payment of Maintenance Fee, 12th Year, Large Entity. |
Date | Maintenance Schedule |
Oct 16 1993 | 4 years fee payment window open |
Apr 16 1994 | 6 months grace period start (w surcharge) |
Oct 16 1994 | patent expiry (for year 4) |
Oct 16 1996 | 2 years to revive unintentionally abandoned end. (for year 4) |
Oct 16 1997 | 8 years fee payment window open |
Apr 16 1998 | 6 months grace period start (w surcharge) |
Oct 16 1998 | patent expiry (for year 8) |
Oct 16 2000 | 2 years to revive unintentionally abandoned end. (for year 8) |
Oct 16 2001 | 12 years fee payment window open |
Apr 16 2002 | 6 months grace period start (w surcharge) |
Oct 16 2002 | patent expiry (for year 12) |
Oct 16 2004 | 2 years to revive unintentionally abandoned end. (for year 12) |